Vertical take-off aircraft provided with canards (1) and primary wings (2), which primary wings (2) are provided with two or more primary thrusters (20). The primary wings (2) are rotatable alternately in a vertical configuration for vertical flight mode and in a horizontal configuration for horizontal flight mode. The canards (1) in said vertical flight mode are arranged substantially parallel to a plane perpendicular to the flight direction, each canard (1) being provided with a secondary thruster (10) oriented for vertical flight mode and at least partially comprised in the profile of the canard (1) itself.
VERTICAL TAKE-OFF AIRCRAFT WITH CANARDS AND PRIMARY WINGS
2024-07-25
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |
VERTICAL TAKE-OFF AIRCRAFT WITH CANARDS AND PRIMARY WINGS
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